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Mahmood, G.I., Gustafson, R. and Acharya, S. (2005) Experimental Investigation of Flow Structure and Nusselt Number in a Low Speed Linear Blade Passage With and Without Leading Edge Fillets. Journal of Heat Transfer, 127, 499-512.
http://dx.doi.org/10.1115/1.1865218

has been cited by the following article:

• TITLE: Computational Study on Effect of Variation of Pitch-Chord on Secondary Losses in Rectilinear Turbine Cascade

  AUTHORS: Pulijala Shravya

  KEYWORDS: Turbine Cascade, Pitch-Chord Ratio, Secondary Losses

  JOURNAL NAME: Engineering, Vol.7 No.11, November 11, 2015

  ABSTRACT: Losses in turbine cascade are categorized as profile loss, secondary loss, tip clearance loss and annulus loss. Profile loss occurs due to development of boundary layer on surface of blade [1]. Increase in thickness of boundary layer and adverse pressure gradient increases profile loss. Secondary loss occurs due to turning of flow through flow passage which results in blowing of energy from pressure side to suction side. In turbine rotor blade suction surface leads and tip clearance loss occurs due to leakage of air from pressure side to suction side of the blade through tip clearance. Annulus loss occurs due to development of boundary layer on stationary row of blade. It also occurs in moving row of blade but in moving row of blades boundary layer is scraped by flow over the blades. This paper presents effects of variation of pitch-chord ratio on secondary loss.